MAULE AIRCRAFT CORPORATION
MAINTENANCE MANUAL
FOR
M-4/C/S/T
1
Rev. B
4/13/16
SECTION I
GENERAL DATA
GENERAL DESCRIPTION:
Type: Four place high wing cabin monoplane.
Engine Installation: Single tractor engine in nose of fuselage.
Wing: Strut braced, two spar, fabric or metal covered, modified USA 35-B airfoil. Fi-
berglass wing tips.
Fuselage: Welded steel tube structure.
Fuselage and tail group covered with fiberglass synthetic fabric. Fiberglass
engine cowl. Aluminum skin on forward fuselage and doors.
Landing Gear: Main gear split axle type, spring-oil oleo shock absorber. Hydraulic
Brakes. Steerable tailwheel (Automatic locking).
Control Systems: Dual controls wheels and rudder pedals. All controls directly cable
driven. Fuel control/shut off valve is at the left lower side panel.
Mechanical flap and trim controls are at the center on the floor. All
other controls, switches, etc., are instrument panel mounted.
DESIGN SPECIFICATIONS:
Wing Span
29 feet 8 inches
Length
22 feet
Height 6 feet 2½ inches
Gross Weight
2100 lbs.*
Empty Weight
Approx. 1136 lbs.
Wing Loading
13.75 lbs./sq. ft.
Power Loading
14.5 lbs./HP
Useful Load
Approx. 964 lbs.
Seats
Four
Flaps
0
°
, 15
°
, 35
°
*
Baggage Allowance
250 lb. Structural Limit
Baggage Compartment Dimensions
30H x 26W x 21L
Wings:
a. Airfoil
Modified USA 35-B
b.
Chord
63 inches
c.
Incidence
+30 minutes
d.
Dihedral
1.2 degrees
e.
Sweepback
None
